CN110553550A - anti-unmanned aerial vehicle net catches device in air - Google Patents
anti-unmanned aerial vehicle net catches device in air Download PDFInfo
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- CN110553550A CN110553550A CN201910836322.2A CN201910836322A CN110553550A CN 110553550 A CN110553550 A CN 110553550A CN 201910836322 A CN201910836322 A CN 201910836322A CN 110553550 A CN110553550 A CN 110553550A
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- net
- umbrella
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- unmanned aerial
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Engineering & Computer Science (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention relates to an air anti-unmanned aerial vehicle net catching device, which sequentially comprises the following parts from the head part to the tail part: a head cabin section, a net cabin section, an umbrella cabin section, a boosting section and a control surface section; the head cabin section comprises a head cover (1), a delay igniter (6), gunpowder (7), a mass block (8) and a body (2); the net cabin section comprises a net box (9) and a flying net (3); the umbrella cabin section comprises a clapboard (4), an umbrella box (10) and a recovery umbrella (5). The recovery umbrella is designed at the rear end of the flying net and is pulled out by the flying net, so that a traction mechanism of the recovery umbrella is omitted, and the recovery of the net capturing device is realized. The net catching device is compact in structure, light in weight, wide in catching range, long in intercepting distance and high in catching precision, and is transmitted by an aerial platform.
Description
Technical Field
The invention belongs to the field of anti-unmanned aerial vehicles, and particularly relates to a net-capture type anti-unmanned aerial vehicle system.
Background
The net catching technology is one of main technologies of an anti-unmanned aerial vehicle system, at present, the research on a net catching device of an anti-unmanned aerial vehicle in foreign countries is mature, the catching and parachuting recovery of the unmanned aerial vehicle can be realized, and the specific details are blocked due to the technology and are not followed. Domestic anti-unmanned aerial vehicle net trapping device generally includes launching mechanism, net rope and power supply, and is less to net trapping device's recovery system relates to, can't realize net trapping device's soft landing and retrieves, and net trapping device generally adopts ground on-vehicle transmission or shoulder carrying formula transmission, and weight is great and the transmission initial velocity is lower, and the interception distance is nearer, catches the precision lower to high altitude unmanned aerial vehicle.
Disclosure of Invention
The purpose of the invention is as follows:
The invention aims to design an aerial emission type anti-unmanned aerial vehicle net catching device aiming at the prior art situation, so as to realize the net catching and recovery of the unmanned aerial vehicle.
the technical scheme adopted by the invention is as follows:
an anti-unmanned aerial vehicle net-catching device comprises a hood 1, a delay igniter 6, a mass block 8, a body 2, gunpowder 7, a net box 9, a flying net 3, a partition plate 4, a recovery umbrella 5, an umbrella box 10, a booster 11 and a control surface section 12;
The net catching device sequentially comprises the following components from the head part to the tail part: a head cabin section, a net cabin section, an umbrella cabin section, a boosting section and a control surface section; the head cabin section comprises a head cover 1, a delay igniter 6, gunpowder 7, a mass block 8 and a body 2; the net cabin section comprises a net box 9 and a flying net 3; the umbrella cabin section comprises a partition plate 4, an umbrella box 10 and a recovery umbrella 5;
The most front end of the net catching device is a head cover 1, a delay igniter 6, gunpowder 7, mass blocks 8 and a body 2 are arranged in the head cover 1, the body 2 is a circular ring-shaped support, the mass blocks 8 are inserted into the body 2 for fixing, the gunpowder 7 is arranged at the front end of the body 2, the delay igniter 6 is fixed on the outer side of the gunpowder 7, the delay igniter 6, the gunpowder 7, the mass blocks 8 and the body 2 form a delay launching mechanism, the delay launching mechanism is arranged at the front end of a net box 9, a flying net 3 is arranged in the net box 9, and the mass blocks 8 are respectively connected with the corners of the flying;
The rear end of the net box 9 is an umbrella box 10, a recovery umbrella 5 is arranged in the umbrella box 10, the flying net 3 is connected with the recovery umbrella 5 through a rope belt, and a flexible clapboard 4 is arranged between the flying net 3 and the recovery umbrella 5 to prevent the flying net 3 and the recovery umbrella 5 from being wound together;
The back end of the umbrella box 10 is a boosting section which is provided with a booster 11 and provides power for the net catching device;
the rear end of the boosting section is a control surface section 12, and the flight stability of the net capture device is maintained.
the aircraft is characterized in that shells of the nose cabin section, the net cabin section, the umbrella cabin section and the control surface section are all thin-wall plastic parts, and the overall weight is light.
It is characterized in that the boosting section adopts a metal shell, and boosting gunpowder is loaded inside the metal shell.
The sealing device is characterized in that the outer ring of the body 2 is provided with 4 side holes 14, and the number of the sealing rings is the same as that of the side holes 14.
The sealing device is characterized in that a plurality of side holes 14 are formed in the outer ring of the body 2, and after sealing rings are installed in sealing grooves 15 of a plurality of mass blocks 8, the mass blocks 8 are inserted into the side holes 14 of the body 2 to be fixed.
It is characterized in that the front end face of the body 2 is provided with an end face hole 13, and gunpowder 7 is loaded in the end face hole 13.
The device is characterized in that the net catching device is driven by an aerial platform to fly and launch.
The device is characterized in that the boosting section provides a larger initial speed for the net capture device, and the control surface section keeps the air attitude of the net capture device stable, so that the net capture device obtains a longer interception distance.
The rear end of the booster 11 is provided with a bolt 16, the front end of the control surface section 12 is provided with a threaded hole 17, and the threaded hole is matched with the bolt 16 at the rear end of the booster 11 to fix the rear end of the boosting section and the control surface section 12.
the invention has the beneficial effects that:
The recovery umbrella is designed at the rear end of the flying net and is pulled out by the flying net, so that a traction mechanism of the recovery umbrella is omitted, and the recovery of the net capturing device is realized. The net catching device is compact in structure, light in weight, wide in catching range, long in intercepting distance and high in catching precision, and is transmitted by an aerial platform.
Drawings
Fig. 1 is an exploded view of the structure of the net capture device.
Fig. 2 is a sectional view of the netting device.
Detailed Description
The invention is described in further detail below with reference to the drawings.
as shown in fig. 1-2, the net catching device for the air anti-unmanned aerial vehicle comprises a head cover 1, a delay igniter 6, a mass block 8, a body 2, gunpowder 7, a net box 9, a flying net 3, a partition plate 4, a recovery umbrella 5, an umbrella box 10, a booster 11 and a control surface section 12;
the net catching device sequentially comprises the following components from the head part to the tail part: a head cabin section, a net cabin section, an umbrella cabin section, a boosting section and a control surface section; except for the boosting section, the outer shell of the net catching device is made of thin-wall plastic parts, so that the whole weight is light, and the boosting section is made of a metal outer shell and internally loaded with boosting gunpowder;
the most front end of the net catching device is a head cover 1, a delay igniter 6, gunpowder 7, a mass block 8 and a body 2 are arranged in the head cover 1, the body 2 is a circular bracket, 4 side face holes 14 are formed in the outer ring of the body 2, a sealing ring is arranged in sealing grooves 15 of the 4 mass blocks 8, the mass block 8 is inserted into the side face holes 14 of the body 2 to be fixed, an end face hole 13 is formed in the front end face of the body 2, the gunpowder 7 is arranged in the end face hole 13, the delay igniter 6 is fixed on the outer side of the gunpowder 7, the delay igniter 6, the gunpowder 7, the mass block 8 and the body 2 form a delay launching mechanism, the delay launching mechanism is arranged at the front end of a net box 9, a flying net 3 is arranged in the net box 9;
the rear end of the net box 9 is an umbrella box 10, a recovery umbrella 5 is arranged in the umbrella box 10, the flying net 3 is connected with the recovery umbrella 5 through a rope belt, and a flexible clapboard 4 is arranged between the flying net 3 and the recovery umbrella 5 to prevent the flying net 3 and the recovery umbrella 5 from being wound together;
The rear end of the umbrella box 10 is a boosting section, the boosting section is provided with a booster 11 for providing power for the net catching device, and the rear end of the booster 11 is provided with a bolt 16;
The rear end of the boosting section is a control surface section 12 which maintains the flight stability of the net capture device, the front end of the control surface section 12 is provided with a threaded hole 17 which is matched with a bolt 16 at the rear end of the booster 11 to fix the rear end of the boosting section and the control surface section 12.
when the umbrella is installed, the net box 9 is connected with the umbrella box 10, the recovery umbrella 5 is put into the umbrella box 10, and the baffle plate 4 is covered on the recovery umbrella; the flying net 3 is connected with the recovery umbrella 5 by a rope belt, then the flying net 3 is arranged in a net box 9, and the corners of the flying net 3 are connected with mass blocks 8. The mass blocks 8 are then respectively mounted in the side holes 14 of the body 2, and the powder 7 and the delay igniter 6 are sequentially mounted in the end holes 13 of the body 5. Then, one end of the assembled body 2 is connected with the net box 9, and then the head cover 1 is connected with the other end of the body 2. Finally, the booster 11 is connected to the umbrella case 10, and the control surface section 12 is screwed into the bolt 16 of the booster 11.
When the net catching device is ignited and launched, the booster 11 works to push the net catching device to accelerate, the delay igniter 6 is electrified, after a certain time delay, the net catching device flies to a position near the target unmanned aerial vehicle, the delay igniter ignites gunpowder at the moment, the mass block 8 is instantaneously accelerated under the action of the gunpowder, the net box 9 is exploded, the flying net 3 is pulled to be continuously unfolded, and the target unmanned aerial vehicle is caught. After the flying net 3 is unfolded, the speed is reduced, the speed difference exists between the recovery umbrella 5 and the flying net 3, the recovery umbrella 5 is pulled out of the umbrella box 10, and the recovery umbrella is unfolded under the action of wind power and slowly descends to a recovery area, so that the net capture system and the captured unmanned aerial vehicle are recovered.
Claims (9)
1. An anti-unmanned aerial vehicle net-catching device in the air comprises a hood (1), a delay igniter (6), a mass block (8), a body (2), gunpowder (7), a net box (9), a flying net (3), a partition plate (4), a recovery umbrella (5), an umbrella box (10), a booster (11) and a control surface section (12);
the net catching device sequentially comprises the following components from the head part to the tail part: a head cabin section, a net cabin section, an umbrella cabin section, a boosting section and a control surface section; the head cabin section comprises a head cover (1), a delay igniter (6), gunpowder (7), a mass block (8) and a body (2); the net cabin section comprises a net box (9) and a flying net (3); the umbrella cabin section comprises a clapboard (4), an umbrella box (10) and a recovery umbrella (5);
The net catching device is characterized in that the head cover (1) is arranged at the forefront end, a delay igniter (6), gunpowder (7), mass blocks (8) and a body (2) are arranged in the head cover (1), the body (2) is a circular ring-shaped support, a plurality of mass blocks (8) are inserted into the body (2) for fixing, the gunpowder (7) is arranged at the front end of the body (2), the delay igniter (6) is fixed on the outer side of the gunpowder (7), the delay igniter (6), the gunpowder (7), the mass blocks (8) and the body (2) form a delay launching mechanism, the delay launching mechanism is arranged at the front end of a net box (9), a flying net (3) is arranged in the net box (9), and the mass blocks (8) are respectively connected with corners;
the rear end of the net box (9) is provided with an umbrella box (10), a recovery umbrella (5) is arranged in the umbrella box (10), the flying net (3) is connected with the recovery umbrella (5) through a rope belt, and a flexible clapboard (4) is arranged between the flying net (3) and the recovery umbrella (5) to prevent the flying net (3) and the recovery umbrella (5) from being wound together;
The rear end of the umbrella box (10) is a boosting section which is provided with a booster (11) and provides power for the net catching device;
the rear end of the boosting section is a control surface section (12) which maintains the flight stability of the net capture device.
2. the net catching device for the overhead unmanned aerial vehicle as claimed in claim 1, wherein the outer shells of the head cabin section, the net cabin section, the parachute cabin section and the rudder surface section are all made of thin-walled plastic parts, so that the overall weight is light.
3. The net catching device for air anti-unmanned aerial vehicles as claimed in claim 2, wherein the boosting section is made of metal shell and is loaded with boosting powder.
4. An airborne unmanned aerial vehicle arresting device according to claim 3, wherein the outer ring of the body (2) is provided with 4 side holes (14), and the number of the sealing rings is the same as that of the side holes (14).
5. An airborne unmanned aerial vehicle arresting device according to claim 3, wherein the outer ring of the body (2) is provided with a plurality of side holes (14), and after the sealing rings are arranged in the sealing grooves (15) of the plurality of mass blocks (8), the plurality of mass blocks (8) are inserted into the side holes (14) of the body (2) for fixation.
6. An airborne anti-unmanned aerial vehicle net catching device as claimed in claim 4 or 5, characterized in that the front end face of the body (2) is provided with a face hole (13), and gunpowder (7) is loaded into the face hole (13).
7. An airborne anti-drone arresting device according to claim 6 characterised in that the arresting device is propelled by the airborne platform for flight and launch.
8. The net capture device for the air anti-unmanned aerial vehicle as claimed in claim 7, wherein the boosting section provides a larger initial speed of the net capture device, and the control surface section keeps the air attitude of the net capture device stable, so that the net capture device can obtain a longer interception distance.
9. an airborne anti-unmanned aerial vehicle net catching device according to claim 8, characterized in that the rear end of the booster (11) is provided with a bolt (16), the front end of the control surface section (12) is provided with a threaded hole (17) which is matched with the bolt (16) at the rear end of the booster (11) to fix the rear end of the booster and the control surface section (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910836322.2A CN110553550A (en) | 2019-09-03 | 2019-09-03 | anti-unmanned aerial vehicle net catches device in air |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910836322.2A CN110553550A (en) | 2019-09-03 | 2019-09-03 | anti-unmanned aerial vehicle net catches device in air |
Publications (1)
| Publication Number | Publication Date |
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| CN110553550A true CN110553550A (en) | 2019-12-10 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN201910836322.2A Pending CN110553550A (en) | 2019-09-03 | 2019-09-03 | anti-unmanned aerial vehicle net catches device in air |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113218251A (en) * | 2021-06-08 | 2021-08-06 | 南京航空航天大学 | Air flying net capturing bomb and working method thereof |
| CN113654407A (en) * | 2021-08-30 | 2021-11-16 | 航宇救生装备有限公司 | A catch net catapult for unmanned aerial vehicle net catches |
| CN113720208A (en) * | 2021-08-30 | 2021-11-30 | 航宇救生装备有限公司 | Unmanned aerial vehicle catches recovery unit |
Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20120210904A1 (en) * | 2008-08-11 | 2012-08-23 | Merems Paul A | Interceptor projectile and method of use |
| US20140138474A1 (en) * | 2012-03-02 | 2014-05-22 | Alliant Techsystems Inc. | Methods and apparatuses for active protection from aerial threats |
| US20150241180A1 (en) * | 2012-11-01 | 2015-08-27 | Raytheon Company | Countermeasure system and method for defeating incoming projectiles |
| CN105711850A (en) * | 2016-01-30 | 2016-06-29 | 上海仪耐新材料科技有限公司 | Net-bullet type intelligent interception system for resisting unmanned aerial vehicle |
| GB2537664A (en) * | 2015-04-22 | 2016-10-26 | David Down Christopher | A system for tangling a vehicle |
| CN106767172A (en) * | 2017-01-23 | 2017-05-31 | 芜湖博高光电科技股份有限公司 | A kind of pickaback portable anti-unmanned aerial vehicle ejecting is soft to injure retracting device |
| CN206362245U (en) * | 2016-12-07 | 2017-07-28 | 华南农业大学 | It is a kind of be used to intercepting small aircraft can return to formula electric power rocket |
| CN107054678A (en) * | 2017-01-18 | 2017-08-18 | 芜湖博高光电科技股份有限公司 | A kind of vehicle-mounted anti-unmanned plane net bullet intercepting system |
| CN107990787A (en) * | 2017-12-05 | 2018-05-04 | 佛山市海科云筹信息技术有限公司 | A kind of anti-UAV system |
| US20180245888A1 (en) * | 2015-08-27 | 2018-08-30 | Airspace Systems Inc. | Interdiction system and method of operation |
| CN108871081A (en) * | 2018-07-03 | 2018-11-23 | 芜湖博高光电科技股份有限公司 | A kind of net bullet capturing unmanned plane |
| US20190100315A1 (en) * | 2017-09-29 | 2019-04-04 | Shawn M. Theiss | Device and method to intercept an aerial vehicle |
| CN109579620A (en) * | 2018-12-06 | 2019-04-05 | 内蒙动力机械研究所 | A kind of unmanned plane flexibility capture systems and application method |
| CN109916225A (en) * | 2019-03-13 | 2019-06-21 | 北京天剑维安科技发展有限公司 | A kind of net for capturing unmanned plane catches bullet |
-
2019
- 2019-09-03 CN CN201910836322.2A patent/CN110553550A/en active Pending
Patent Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20120210904A1 (en) * | 2008-08-11 | 2012-08-23 | Merems Paul A | Interceptor projectile and method of use |
| US20140138474A1 (en) * | 2012-03-02 | 2014-05-22 | Alliant Techsystems Inc. | Methods and apparatuses for active protection from aerial threats |
| US20150241180A1 (en) * | 2012-11-01 | 2015-08-27 | Raytheon Company | Countermeasure system and method for defeating incoming projectiles |
| GB2537664A (en) * | 2015-04-22 | 2016-10-26 | David Down Christopher | A system for tangling a vehicle |
| US20180245888A1 (en) * | 2015-08-27 | 2018-08-30 | Airspace Systems Inc. | Interdiction system and method of operation |
| CN105711850A (en) * | 2016-01-30 | 2016-06-29 | 上海仪耐新材料科技有限公司 | Net-bullet type intelligent interception system for resisting unmanned aerial vehicle |
| CN206362245U (en) * | 2016-12-07 | 2017-07-28 | 华南农业大学 | It is a kind of be used to intercepting small aircraft can return to formula electric power rocket |
| CN107054678A (en) * | 2017-01-18 | 2017-08-18 | 芜湖博高光电科技股份有限公司 | A kind of vehicle-mounted anti-unmanned plane net bullet intercepting system |
| CN106767172A (en) * | 2017-01-23 | 2017-05-31 | 芜湖博高光电科技股份有限公司 | A kind of pickaback portable anti-unmanned aerial vehicle ejecting is soft to injure retracting device |
| US20190100315A1 (en) * | 2017-09-29 | 2019-04-04 | Shawn M. Theiss | Device and method to intercept an aerial vehicle |
| CN107990787A (en) * | 2017-12-05 | 2018-05-04 | 佛山市海科云筹信息技术有限公司 | A kind of anti-UAV system |
| CN108871081A (en) * | 2018-07-03 | 2018-11-23 | 芜湖博高光电科技股份有限公司 | A kind of net bullet capturing unmanned plane |
| CN109579620A (en) * | 2018-12-06 | 2019-04-05 | 内蒙动力机械研究所 | A kind of unmanned plane flexibility capture systems and application method |
| CN109916225A (en) * | 2019-03-13 | 2019-06-21 | 北京天剑维安科技发展有限公司 | A kind of net for capturing unmanned plane catches bullet |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113218251A (en) * | 2021-06-08 | 2021-08-06 | 南京航空航天大学 | Air flying net capturing bomb and working method thereof |
| CN113218251B (en) * | 2021-06-08 | 2022-07-26 | 南京航空航天大学 | Air flying net capturing bomb and working method thereof |
| CN113654407A (en) * | 2021-08-30 | 2021-11-16 | 航宇救生装备有限公司 | A catch net catapult for unmanned aerial vehicle net catches |
| CN113720208A (en) * | 2021-08-30 | 2021-11-30 | 航宇救生装备有限公司 | Unmanned aerial vehicle catches recovery unit |
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Application publication date: 20191210 |